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6. ****
2. Manufacturer and manufacturer's
designation of aircraft**
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CHAPTER 4. CONTINUING AIRWORTHINESS OF AIRCRAFT
4.1 Applicability
The Standards of this chapter are applicable to all aircraft.
4.2 Responsibilities of Contracting States
in respect of continuing airworthiness
Note.- Guidance on continuing airworthiness requirements
is contained in the Airworthiness Manual (Doc 9760).
4.2.1 State of Design
4.2.1 .I The State of Design of an aircraft shall:
a) transmit to every Contracting State which has in accordance
with 4.2.3 a) advised the State of Design that it
has entered the aircraft on its register, and to any other
Contracting State upon request, any generally applicable
information which it has found necessary for the
continuing airworthiness of the aircraft, including its
engines and propellers when applicable, and for the safe
operation of the aircraft, (hereinafter called mandatory
continuing airworthiness information) and notification
of the suspension or revocation of a Type Certificate;
Note I.- The term "mandatory continuing ainuorthiness
information" is intended to include mandatory
requirements for modification, replacement of parts or
inspection of aircraji and amendment of operating limitations
and procedures. Among such infinnation is that
issued by Contracting States in the form of ainuorthiness
directives.
Note 2.- The Continuing Airworthiness of Aircraft
in Service (Cir 95) provides the necessary information
to assist Contracting States in establishing contact with
competent authorities of other Contracting States for
the purpose of maintaining continuing airworthiness of
aircraft in service.
b) ensure that, in respect of aeroplanes over 5 700 kg and
helicopters over 3 175 kg maximum certificated takeoff
mass, there exists a system for:
i) receiving information submitted in accordance with
4.2.3 f);
ii) deciding if and when airworthiness action is needed;
iii) developing the necessary airworthiness actions; and
iv) promulgating the information on those actions
including that required in 4.2.1.1 a);
c) ensure that, in respect of aeroplanes over 5 700 kg
maximum certificated take-off mass, there exists a
continuing structural integrity programme to ensure the
airworthiness of the aeroplane. The programme shall
include specific information concerning corrosion
prevention and control; and
d) ensure that, where the State of Manufacture of an
aircraft is other than the State of Design, there is an
agreement acceptable to both States to ensure that the
manufacturing organization cooperates with the organization
responsible for the type design in assessing
infortnation received on experience with operating the
aircraft.
4.2.1.2 The State of Design of an engine or a propeller,
where it is different from the State of Design of the aircraft,
shall transmit any continuing airworthiness information to the
State of Design of the aircraft and to any other Contracting
State upon request.
4.2.2 State of Manufacture
The State of Manufacture of an aircraft shall ensure that where
it is not the State of Design there is an agreement acceptable
to both States to ensure that the manufacturing organization
cooperates with the organization responsible for the type
design in assessing information received on experience with
operating the aircraft.
4.2.3 State of Registry
The State of Registry shall:
a) ensure that, when it first enters on its register an aircraft
of a particular type for which it is not the State of
Design and issues or validates a Certificate of Airworthiness
in accordance with 3.2 of this part, it shall
advise the State of Design that it has entered such an
aircraft on its register;
b) determine the continuing airworthiness of an aircraft in
relation to the appropriate airworthiness requirements in
force for that aircraft;
ANNEX 8 11-4-1 13/12/07
Annex 8 -Airworthiness of Aircraji Part ZZ
c) develop or adopt requirements to ensure the continuing
airworthiness of the aircraft during its service life,
including requirements to ensure that the aircraft:
i) continues to comply with the appropriate airworthiness
requirements after a modification, a repair or the
installation of a replacement part; and
ii) is maintained in an airworthy condition and in compliance
with the maintenance requirements of
Annex 6, and where applicable, Parts 111, IV and V of
this Annex;
d) upon receipt of mandatory continuing airworthiness
　
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